Summary The aircraft, a Cosmos Phase II ES ultralight, registration C-IFEK, serial number 21221, took off from a private gravel runway at Saint-Mathias-de-Richelieu, Quebec, for a familiarization flight with one passenger on board as part of an air show. Shortly after take-off, around 1730 local time, the pilot departed from the circuit that had been used since the beginning of the show's activities. The aircraft was flying at low altitude when it banked sharply and struck the ground. The pilot and the passenger sustained fatal injuries. Ce rapport est galement disponible en franais. Other Factual Information The pilot held an ultralight aircraft licence with an instructor rating valid until May 2004. He had accumulated almost 60 hours' flying time, all on the Cosmos Phase II ES. As an instructor, he could give dual training on ultralight aircraft. Based on the autopsy and toxicological test results, there is no indication that physiological factors affected the pilot's performance. Specific procedures had been established for the circuit for the show. After taking off from runway 13, the instructor was to proceed towards Chambly Basin, west of the airport, and then turn left to fly over highway 10 until he joined the base leg for runway 13. The trip was to last about 15 minutes, during which the instructor was to initiate the passenger into flying an ultralight aircraft by demonstrating manoeuvres normally performed as part of a familiarization flight, such as the various aircraft attitudes. The term familiarization flight is borrowed here from the instructor's guide for conventional aircraft, because the term is not defined and the lessons are not structured in the ultralight field. Several persons made ultralight flights at a preset rate during the weekend festivities. The purpose of these flights was to introduce the passengers to ultralight flying and possibly get them to enrol in a complete training course at the Cosmos U.L.M. Inc. training centre. The purpose of the flights, among other things, was to recruit new students. At the time of the occurrence, the sky was clear. At 1700 local time, at the Saint-Hubert airport, Quebec, located about 10 miles northwest of the town, the winds were from 280 degrees magnetic at 9 knots gusting to 18 knots. At 1800 local time, the winds were from 270 degrees magnetic at 14 knots. Such winds can produce low-level mechanical turbulence. Shortly before the flight, a company maintenance engineer made a check and indicated that everything was normal. The aircraft took off normally, proceeded away from Chambly Basin, flew over a hangar, and crashed near a heavy vehicle. Nearby, there were large fields bordered by big trees. The investigation revealed that the minimum descent gradient at the time of impact would have been greater than 45 degrees and that the engine was producing power at the time of impact. These motorized ultralights are manufactured by the French company Cosmos, which provides a considerable amount of information on its product and makes technical manuals available to its clients. The manufacturer suggests assembly procedures, with information on techniques and the sequence of assembly. The user's manual provides the aircraft's performance data and available options. The maintenance manual also provides the aircraft's performance data and its handling characteristics. In addition, the manual sets out a schedule of maintenance and inspections to be carried out at various intervals. It was not possible to determine whether the flying school followed this maintenance schedule, because no relevant records were found. Canadian regulations do not require operators of ultralight aircraft to keep such records. Several aircraft parts were sent to the TSB Engineering Branch Laboratory to determine whether the fractures identified were caused by the impact with the ground or whether the fractures had occurred before impact. A microscopic examination of the attachments and the fractures identified on some parts was carried out at the TSB Laboratory. The examination revealed that the fractures were attributable to the violent impact with the ground.